Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, 3, Performance Characteristics with the High-Flow Compressor

Author: Fleming, William A.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E8F09b
Link: https://digital.library.unt.edu/ark:/67531/metadc63839/

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